View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 7210U 74011B 24358.17736801 .00000137 00000-0 63405-4 0 9991
2 7210 81.2356 238.3962 0081144 127.4031 233.4564 14.13487672617808
| Epoch (UTC): | 23 December 2024 04:15:24 |
| Eccentricity: | 0.0081144 |
| inclination: | 81.2356° |
| perigee height: | 789 km |
| apogee height: | 906 km |
| right ascension of ascending node: | 238.3962° |
| argument of perigee: | 127.4031° |
| revolutions per day: | 14.13487672 |
| mean anomaly at epoch: | 233.4564° |
| orbit number at epoch: | 61780 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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